[0001] The present invention relates to a low alloy steel for generator rotor shafts, which
has excellent magnetic properties.
[0002] There have been known materials for rotor shafts, on which a magnetic field winding
is mounted, such steels as shown in
JP-B2-47-25248 and
JP-B2-50-7530. In particular, as a generator shaft material necessitating not lower than 700 MPa
of tensile strength at room temperature, a steel containing not less than 3.0% nickel
and not more than 2.0% chromium as disclosed in ASTM Standard A469 has generally been
used.
[0003] Conventionally, as a rotor shaft material for a comparatively large size generator
driven by a gas turbine or a steam turbine, a low alloy steel containing not less
than 3.0% nickel has been used. However, such low alloy steel for generator rotor
shafts containing the above range of nickel is inferior in magnetic properties. As
a result, the efficiency of the generator decreases. On the other hand, since nickel
is an essential component for improving the low alloy steel in harden ability although
deteriorating magnetic properties, it has been difficult to reduce the nickel amount.
[0004] Accordingly, an object of the present invention is to provide a low alloy steel for
generator rotor shafts, which low alloy steel contains a lower amount of nickel than
those in conventional low alloy steels, and has improved magnetic properties and realizable
harden ability.
[0005] Another object of the present invention is to provide a low alloy steel for generator
rotor shafts, which low alloy steel has not lower than 700 MPa of tensile strength
at room temperature, not higher than 275 AT/m of magnetizing force at room temperature,
and not higher than 7°C of FATT,
[0006] Under the above objects, there is provided a low alloy steel for generator rotor
shafts, which low alloy steel contains a reduced amount of nickel, an increased amount
of chromium, and additive copper.
[0007] Specifically the low alloy steel contains, by mass percent, a primary component of
Fe, 1.3 to 2.0% Ni, 2.1 to 3.0% Cr, and 0.15 to 0.35% Cu.
[0008] More specifically the low alloy steel consists essentially of, by mass percent, 0,15
to 0,35% carbon, 0.01 to 0.10% Si, 0.10 to 0.50 Mn, 1.3 to 2.0 Ni, 2.1 to 3.0% Cr,
0.20 to 0.50% Mo, 0.15 to 0,35% Cu, 0.06 to 0.14% V, and the balance of Fe and unavoidable
impurities.
[0009] According to the invention low alloy steel for generator rotor shafts, it is possible
to reduce a field current allowing to pass in a coil of generator rotor since the
low alloy steel is excellent in magnetic properties, so that the loss of the generator
decreases thereby enabling the generation efficiency improved.
Detailed description of the invention
[0010] If the nickel amount of the low alloy steel s for generator rotor shafts is reduced,
those harden ability will be deteriorated. Thus, a low alloy steel containing not
less than 3.0% nickel has been used. The present inventors made researches on the
harden ability of low alloy steels, and found that in the case where the nickel amount
of those is reduced to a specific range, they can have a quench effect equivalent
to that of a low alloy steel containing not less than 3.0% nickel by adding proper
amounts of chromium and copper. Further, the inventors found that by manufacturing
a generator with use of a generator rotor shaft material of a thus obtained alloy
in which the nickel amount is made lower than that of conventional materials, the
magnetic properties of the generator are improved as compared with conventional generators
thereby improving the generation efficiency.
[0011] Hereinbelow, there will be provided a description of functions of the additive elements
in the alloy of rotor shafts and reasons why the composition ranges of the elements
are preferred.
[0012] Carbon is an indispensable element in order to improve harden ability and strength
of the generator rotor shaft material, so that the low alloy steel needs it in an
amount of not less than 0,15%. However, if the carbon amount exceeds 0.35%, toughness
of the generator rotor shaft material is deteriorated. Therefore, the carbon amount
is set to be 0,15 to 0.35%, preferably 0.20 to 0.30%.
[0013] Silicon has a deoxidizing effect, so that it has been added to generator rotor shaft
materials as an element for improving the cleanliness of thereof. In recent years,
by virtue of the progress of steel manufacturing technique such as the carbon deoxidation
method under vacuum, a sound generator rotor shaft material can be produced by melting
without additive silicon. From the viewpoint of prevention of temper embrittlement,
the silicon amount should be a lower level, that is, within the range of 0.01 to 0,10%.
Manganese is an indispensable element in order to improve harden ability and toughness
of the generator rotor shaft material, so that the material needs it in an amount
of not less than 0.1 %. However, if the manganese amount exceeds 0.50%, there will
occur temper embrittlement of the generator rotor shaft material. Therefore, the manganese
amount is set to be 0.10 to 0.50%, preferably 0.20 to 0.45%.
[0014] Nickel is an indispensable element in order to improve the generator rotor shaft
material in harden ability, toughness of a central section of the material, and magnetic
properties, so that the material needs it in an amount of not less than 1.3%. However,
if the nickel amount exceeds 2.0%, the magnetic properties of the generator rotor
shaft material are deteriorated. Therefore, the nickel amount is set to be 1.3 to
2.0%, preferably 1.4 to 1.8%.
[0015] Chromium is an indispensable element in order to improve harden ability and strength,
and toughness of the central section of the generator rotor shaft material, so that
the material needs not less than 2.1 % of chromium. However, if the nickel amount
exceeds 3.0%, the generator rotor shaft material is deteriorated in strength. Therefore,
the chromium amount is set to be 2.1 to 3.0%, preferably 2.3 to 2.8%,
[0016] Molybdenum is an indispensable element in order to improve the generator rotor shaft
material in harden ability, and toughness of the central portion of the material,
and to alleviate temper embrittlement, so that the material needs not less than 0.2%
of molybdenum, However, if the molybdenum amount exceeds 0.5%, the generator rotor
shaft material is deteriorated in magnetic properties, Therefore, the molybdenum amount
is set to be 0.20 to 0.50%, preferably 0.30 to 0.40%.
[0017] Copper is an indispensable element in order to improve harden ability, and toughness
of the central section of the generator rotor shaft material, so that the material
needs not less than 0.15% of copper. However, if the copper amount exceeds 0.35%,
the generator rotor shaft material is deteriorated in forgeability. Therefore, the
copper amount is set to be 0.15 to 0.35%, preferably 0.20 to 0.30%.
[0018] Vanadium heightens yield stress of the generator rotor shaft material by forming
carbide particles to cause crystal grains fine, so that the material needs not less
than 0.06% of vanadium. However, if the vanadium amount exceeds 0.14%, the generator
rotor shaft material is deteriorated in toughness. Therefore, the vanadium amount
is set to be 0.06 to 0.14%, preferably 0.08 to 0.12%.
[0019] The unavoidable impurities may be Al, P, S, Sn, Sb, As, and so on. The Al amount
should be a lower level because aluminum deteriorates the material in toughness. The
Al amount is preferably not more than 0.012%. The sulfur amount should be a lower
level because sulfur forms inclusion MnS to deteriorate the material in toughness.
The sulfur amount is preferably not more than 0.015%. The amounts of P, Sn, Sb, As
and so on should be lower because these elements are liable to generate temper embrittlement
of the material. Preferably, the P amount is not more than 0.020%, the Sn amount is
not more than 0.015%, the Sb amount is not more than 0.004%, and the As amount is
not more than 0.015%.
[0020] The invention low alloy steel material for generator rotor shafts may be produced
by the following process:
- (1) A melt of the material prepared by means of an electric furnace, and thereafter
the melt is refined by a vacuum degassing process, a carbon deoxidation process under
vacuum or an electroslag remelting process;
- (2) the thus produced melt is cast into a die to produce an ingot;
- (3) the ingot is subjected to hot forging at a temperature of not lower than 1150°C,
subsequent normalizing at a temperature of not lower than 840°C, and subsequent tempering
at a temperature of not lower than 600°C to make crystal grains fine; and
- (4) subsequently the thus obtained material is subjected to austenitizing at a temperature
of 860 to 900°C, subsequent quenching, such as water cooling, water jet cooling or
water spray cooling, and subsequent tempering at a temperature of 560 to 660°C to
adjust mechanical properties of the material.
- Fig. 1
- is a graph showing the relationship between the nickel amount and the magnetizing
force;
- Fig. 2
- is a graph showing the relationship between the chromium amount and the tensile strength;
- Fig. 3
- shows a generator rotor shaft as one embodiment of the present invention; and
- Fig. 4
- is a general view of a generator which includes a generator rotor shaft with use of
the invention material.
[0021] Embodiments of the invention will be discussed in the following in conjunction with
the accompanying drawings.
Embodiments:
[0022] Hereinbelow, there will be provided a description of embodiments of the invention
low alloy steel material for generator rotor shafts. Table 1 shows the chemical compositions
(mass%) of specimen steels. Specimen steel Nos. 3 to 7 and 9 to 14 are of embodiments
of the present invention. Specimen steel Nos. 1, 2 and 8 are of comparative materials
produced through melting for the comparison purpose. Specimen No. 1 corresponds to
Class 7 of ASTM Standard A469 concerning generator rotor shaft materials.
Table 1
| |
Specimen Steel No. |
Fe |
C |
Si |
Mn |
Ni |
Cr |
Mo |
V |
Cu |
Al |
P |
S |
Sn |
Sb |
As |
| Comparative material |
1 |
Balance |
0.22 |
0.05 |
0.29 |
3.47 |
1.67 |
0.39 |
0.10 |
0.02 |
0.002 |
0.005 |
0.001 |
0.0025 |
0.0009 |
0.0030 |
| Comparative material |
2 |
Balance |
0.27 |
0.04 |
0.26 |
1.16 |
3.12 |
0.36 |
0.09 |
0.20 |
0.005 |
0.007 |
0.004 |
|
|
|
| Invention material |
3 |
Balance |
0.28 |
0.07 |
0.27 |
1.30 |
2.64 |
0.37 |
0.10 |
0.21 |
0.004 |
0.011 |
0.003 |
|
|
|
| Invention material |
4 |
Balance |
0.30 |
0.03 |
0.26 |
1.43 |
2.62 |
0.38 |
0.11 |
0.25 |
0.005 |
0.014 |
0.004 |
|
|
|
| Invention material |
5 |
Balance |
0.26 |
0.03 |
0.29 |
1.67 |
2.56 |
0.35 |
0.10 |
0.27 |
0.006 |
0.013 |
0.007 |
0.0060 |
0.0012 |
0.0061 |
| Invention material |
6 |
Balance |
0.24 |
0.04 |
0.28 |
1.79 |
2.52 |
0.34 |
0.12 |
0.26 |
0.003 |
0.021 |
0.006 |
|
|
|
| Invention material |
7 |
Balance |
0.26 |
0.01 |
0.27 |
1.98 |
2.50 |
0.36 |
0.11 |
0.28 |
0.004 |
0.009 |
0.005 |
|
|
|
| Comparative material |
8 |
Balance |
0.21 |
0.02 |
0.22 |
2.26 |
2.01 |
0.35 |
0.10 |
0.30 |
0.005 |
0.007 |
0.003 |
|
|
|
| Invention material |
9 |
Balance |
0.22 |
0.05 |
0.36 |
1.65 |
2.11 |
0.31 |
0.12 |
0.27 |
0.007 |
0.008 |
0.006 |
|
|
|
| Invention material |
10 |
Balance |
0.20 |
0.04 |
0.45 |
1.68 |
2.21 |
0.34 |
0.12 |
0.25 |
0.009 |
0.007 |
0.004 |
|
|
|
| invention material |
11 |
Balance |
0.24 |
0.09 |
0.32 |
1.60 |
2.41 |
0.30 |
0.11 |
0.23 |
0.006 |
0.006 |
0.005 |
0.0036 |
0.0013 |
0.0083 |
| Invention material |
12 |
Balance |
0.21 |
0.07 |
0.28 |
1.62 |
2.69 |
0.34 |
0.08 |
0.24 |
0.005 |
0.008 |
0.003 |
|
|
|
| Invention material |
13 |
Balance |
0.26 |
0.10 |
0.20 |
1.64 |
2.79 |
0.40 |
0.09 |
0.27 |
0.007 |
0.006 |
0.006 |
|
|
|
| Invention material |
14 |
Balance |
0.26 |
0.06 |
0.24 |
1.67 |
2.97 |
0.36 |
0.09 |
0.26 |
0.003 |
0.009 |
0.004 |
|
|
|
[0023] Each of the specimen steels was prepared by the following process:
- (1) A 20kg ingot was produced by casting a melt of steel prepared by a melting furnace.
- (2) The ingot is subjected to hot forging at a temperature of 1150 to 1250°C to make
a product having a thickness of 30mm and a width of 90mm.
- (3) The product is subjected to a heat treatment simulating a cooling rate of a central
section of a rotor shaft body in a large size generator, which heat treatment includes
normalizing at a temperature of 900°C, heating the work up to 880°C for austenitizing,
quenching the work from the temperature of 880°C at a cooling rate of 200°C/hour,
tempering at a temperature of 600 to 640°C for 33 hours, and cooling to room temperature
at a cooing rate of 30°C/hour in this order, wherein the tempering treatment was conducted
by selecting a temperature such that obtained tensile strength of the work was within
a range of not lower than 700 MPa for each specimen steel.
[0024] Each of the specimen steels subjected to the above heat treatment was subjected to
a tensile test, a 2mm V-notch Charpy impact test, and a DC magnetic property test.
The tensile test was conducted at room temperature with use of a reduced size (5mm
diameter) No. 4 test piece of JIS Z 2201. The 2mm V-notch Charpy impact test was conducted
in a temperature range of -80 to +40°C with use of a V-notch test piece of JIS Z 2202.
The DC magnetic property test was conducted at room temperature with use of a test
piece having a diameter of 200mm and a length of 45 mm by the method specified in
JIS C 2501 (a closed magnetic circuit is formed by an electromagnet and a test piece),
The test results are shown in Table 2. FATT denotes a transition temperature through
which there arises a transformation between a ductile fracture surface and a brittle
fracture surface obtained by the impact test. The lower the value of FATT temperature,
the higher the toughness of steel. In the DC magnetic property test, a magnetizing
force was determined when a magnetic flux density reaches 21.2 kG (kilogauss). As
the value of magnetizing force increases, the steel is excellent in magnetic property.
Table 2
| |
Specimen Steel No. |
Tensile strength (MPa) |
0.02% proof stress (MPa) |
Elongation (%) |
Reduction of area (%) |
FATT(°C) |
Magnetizing force (AT/cm) |
| Comparative material |
1 |
879 |
716 |
21 |
64 |
-20 |
351 |
| Comparative material |
2 |
745 |
588 |
23 |
61 |
10 |
297 |
| Invention material |
3 |
748 |
590 |
22 |
63 |
4 |
267 |
| Invention material |
4 |
750 |
592 |
24 |
62 |
-1 |
251 |
| invention material |
5 |
753 |
595 |
23 |
65 |
-5 |
248 |
| Invention material |
6 |
755 |
596 |
23 |
63 |
-8 |
254 |
| Invention material |
7 |
757 |
598 |
22 |
62 |
-12 |
267 |
| Comparative material |
8 |
761 |
600 |
23 |
64 |
-15 |
286 |
| Invention material |
9 |
701 |
554 |
22 |
61 |
12 |
247 |
| Invention material |
10 |
726 |
574 |
21 |
63 |
7 |
245 |
| Invention material |
11 |
751 |
593 |
22 |
60 |
-3 |
249 |
| Invention material |
12 |
746 |
589 |
23 |
64 |
-17 |
247 |
| Invention material |
13 |
735 |
581 |
21 |
63 |
-22 |
246 |
| Invention material |
14 |
704 |
556 |
22 |
62 |
-32 |
248 |
[0025] As will be appreciated from Table 2, the invention specimens, having preferable alloy
compositions, have not lower than 700 MPa of tensile strength, not higher than 275
AT/m of a magnetizing force, and not higher than 7°C of the FATT. Since generator
rotor shafts rotate at 3000 to 3600 rpm, and repeats start and stop everyday, especially
a slot section must be designed so as to withstand tensile stress occurred by a rotation
centrifugal force. If the tensile stress exceeds the 0.02% proof stress in the slot
section of a generator rotor shaft, there will arise problems such that plastic deformation
is liable to occur, and fatigue fracture is liable to occur due to repeating stress
fluctuation. Also, in the case where the values of elongation and reduction of area
are low, the fracture toughness is low, and the fatigue fracture is liable to occur.
[0026] Fig. 1 shows an influence of nickel amount on the magnetizing force when the magnetic
flux density reaches 21.2 kG. As shown in Fig.1, the magnetizing force is low when
the nickel amount is in the range of 1.3 to 2.0%. Therefore, the nickel amount should
be in the range of 1.3 to 2.0%.
[0027] Fig. 2 shows an influence of chromium amount on tensile strength at room temperature.
As shown in Fig. 2, not lower than 700 MPa of tensile strength at room temperature
is attained when the chromium amount is in the range of 2.1 to 3.0%. Therefore, the
chromium amount should be in the range of 2.1 to 3.0%. As shown in Table 2, the invention
specimen steels have not higher than 7°C of FATT, so that the toughness of the central
section is also excellent.
[0028] Fig. 3 is a perspective view showing one example of a generator rotor shaft. The
rotor shaft shown in Fig. 3 has a magnetic pole 1, a coupling 2, fan mounting rings
3, centering rings 4, slots 5, and tooth 6. The invention material is most suitably
applied to the magnetic pole 1, the coupling 2, and the tooth 6, for example.
[0029] Fig. 4 is a general view of a generator. The whole of the generator shown in Fig.
4 has a generator rotor shaft 7, a rotor coil 8, a retaining ring 9, a collector ring
brush 10, a fan 11, a bearing 12, a stator coil 13, an iron core 14, a stator frame
15, and a high-voltage bushing 16.
[0030] It should be further understood by those skilled in the art that although the foregoing
description has been made on embodiments of the invention, the invention is not limited
thereto and various changes and modifications may be made without departing from the
spirit of the invention and the scope of the appended claims.
[0031] The invention low alloy steel for generator rotor shafts is used as a generator rotor
shaft material which is driven by a gas turbine or a steam turbine. In particular,
it is used as a rotor shaft material having a tensile strength not lower than 700
MPa at room temperature,
[0032] List of reference signs
- 1
- a magnetic pole
- 2
- a coupling
- 3
- fan mounting ring
- 4
- centering rings
- 5
- slots
- 6
- tooth
- 7
- a generator rotor shaft
- 8
- a rotor coil
- 9
- a retaining ring
- 10
- a collector ring brush
- 11
- a fan
- 12
- a bearing
- 13
- a stator coil
- 14
- an iron core
- 15
- a stator frame
- 16
- a high-voltage bushing
1. A low alloy steel for generator rotor shafts, comprising, by mass percent, a primary
component of Fe, 1.3 to 2.0% Ni, 2.1 to 3.0% Cr, and 0.15 to 0.35% Cu.
2. The low alloy steel according to claim 1, which has tensile strength of not less than
700 MPa at room temperature.
3. A low alloy steel for generator rotor shafts, consisting essentially of, by mass percent,
0.15 to 0.35% carbon, 0.01 to 0.10% Si, 0.10 to 0.50% Mn, 1.3 to 2.0% Ni, 2.1 to 3.0%
Cr, 0.20 to 0.50% Mo, 0.15 to 0.35% Cu, 0.06 to 0.14% V, and the balance of Fe and
unavoidable impurities.
4. The low alloy steel according to claim 3, which has tensile strength of not less than
700 MPa at room temperature.
5. Generator with use of a rotor shaft made of the low alloy steel as defined in claim
1,
6. Generator with use of a rotor shaft made of the low alloy steel as defined in claim
3.